U.S. patent application number 12/462905 was filed with the patent office on 2010-02-18 for array of aircraft seats.
Invention is credited to Anthony Harcup.
Application Number | 20100038485 12/462905 |
Document ID | / |
Family ID | 41680615 |
Filed Date | 2010-02-18 |
United States Patent
Application |
20100038485 |
Kind Code |
A1 |
Harcup; Anthony |
February 18, 2010 |
Array of aircraft seats
Abstract
Sleeper seats, wherein each comprises a head rest, a back rest,
a seat pan or seat cushion, a leg rest, an ottomans and a dividers
between the individual seats with the their column. The four seats
are arranged in a staggered chevron formation and two columns. All
the seats in each column are parallel with each other and set at a
"herringbone" angle .alpha. to the column direction, in other words
their central axes A make the angle .alpha. with a longitudinal
axis of the array. Each seat extends from its column side of the
longitudinal axis across the axis to a small extent. Along the
axis, first a seat from one column crosses the axis and then a seat
from the other column crosses the axis and so on.
Inventors: |
Harcup; Anthony; (London,
GB) |
Correspondence
Address: |
LAMBERT & ASSOCIATES, P.L.L.C.
92 STATE STREET
BOSTON
MA
02109-2004
US
|
Family ID: |
41680615 |
Appl. No.: |
12/462905 |
Filed: |
August 11, 2009 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
|
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61188568 |
Aug 11, 2008 |
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Current U.S.
Class: |
244/118.6 |
Current CPC
Class: |
B64D 11/06 20130101;
B64D 11/0601 20141201; B64D 11/0604 20141201 |
Class at
Publication: |
244/118.6 |
International
Class: |
B64D 11/06 20060101
B64D011/06 |
Claims
1. An array of aircraft seats comprising: two columns of seats
arranged for array along an aircraft cabin on respective sides of a
longitudinal axis of the array; the seats having respective central
axes, the seats in each column having their central axes angled
with respect to the longitudinal axis, the seats in one column
being offset along the longitudinal axis with respect to the
corresponding seats in the other column, whereby the intersections
with the longitudinal axis of the central axes of the seats of one
column are interdigitated with the intersections with the
longitudinal axis of the central axes of the seats of the other
column and minor, overlapping, inner-end portions of any two seats
arranged for-and-aft of each other in one column extending across
the longitudinal axis from their major portions at their
intersections and an intervening seat in the other column having a
minor, overlapping, inner-end portion extending oppositely across
the longitudinal axis from its major portion at its intersection;
and a serpentine divider extending generally along the longitudinal
axis between the seats of the two columns, following the extent of
the minor overlapping portions across the longitudinal axis.
2. An array of aircraft seats according to claim 1, wherein the
minor, overlapping, inner-end portions of the two columns overlap
the longitudinal axis by equal extents.
3. An array of aircraft seats according to claim 1, wherein the
extent of the overlap of the minor, overlapping, inner-end portions
is between 3% and 6% of the overall width of the array.
4. An array of aircraft seats according to claim 1, wherein all the
seats are arranged with their central axes at substantially the
same angle with respect to the longitudinal axis.
5. An array of aircraft seats according to claim 4, wherein the
seats are arranged in a staggered chevron array, that is with the
seats in one column angled with respect to the seats in the other
column, and with the central axes of all the seats in one column
making with the longitudinal axis substantially the same angle
measured in the clockwise (or anti-clockwise) direction as the
central axes of all the seats in the other column make with the
longitudinal axis measured in the anti-clockwise (or clockwise)
direction.
6. An array of aircraft seats according to claim 5, wherein the
seats are all arranged to face outwards from the longitudinal axis,
the inner-ends of the seats being head ends thereof.
7. An array of aircraft seats according to claim 6, wherein the
seats are all arranged to face forwards of the aircraft cabin in
which they are to be arrayed.
8. An array of aircraft seats according to claim 5, wherein the
seats are all arranged to face in towards the longitudinal axis,
the inner-ends of the seats being foot ends thereof.
9. An array of aircraft seats according to claim 4, wherein the
seats in one column are arranged substantially parallel with the
seats in the other column, that is with the central axes of all the
seats in both columns making with the longitudinal axis
substantially the same angle measured in the clockwise (or
anti-clockwise) direction.
10. An array of aircraft seats according to claim 9, wherein each
seat in one column is aligned with an opposite facing seat in the
other column, i.e. their central axes are coincident.
11. An array of aircraft seats according to claim 9, wherein each
seat in one column is offset from an opposite facing seat in the
other column, i.e. their central axes are offset from each
other.
12. An array of aircraft seats according to claim 1, including at
least one further column of seats spaced by an aisle from the
neighbouring one of the two columns of seats: the seats of the
further column having respective central axes and the seats in the
further column having their central axes angled with respect to the
longitudinal axis.
13. An array of aircraft seats according to claim 11, wherein the
seats of the or each further column are outwards and forwards
facing.
14. An array of aircraft seats according to claim 1, wherein the
seats are sleeper seats.
15. An array of aircraft seats according to claim 1, including
dividers between the seats, the serpentine divider being comprised
of successive longitudinal axis portions of the dividers between
the seats.
Description
CROSS REFERENCE TO RELATED APPLICATION
[0001] This application takes priority from and claims the benefit
of Provisional Application Ser. No. 61/188,568 filed on Aug. 11,
2008 the contents of which are hereby incorporated by
reference.
BACKGROUND OF THE INVENTION
[0002] 1. Field of the Invention
[0003] The present invention relates to an array of aircraft
seats.
[0004] 2. Description of the Related Art
[0005] Aircraft passenger seats are arrayed in an aircraft cabin in
accordance with a Layout of Passenger Accommodation, known in the
art as a LOPA. A LOPA generally refers to the layout for an entire
aircraft and includes not only seating, but also galleys and
lavatories. The present invention relates to an array primarily,
but not exclusively, for sleeper seats; that is seats that are
convertible from sitting mode to sleeping mode. Such seats usually
comprise a proportion only of the total seating in a cabin.
Accordingly in this specification, the term "array of aircraft
seats" of aircraft seats is used to denote arrangement of a
proportion, or indeed possibly the totality, the seats in an
overall LOPA.
[0006] In design of a LOPA, a major consideration is efficient
utilisation of the cabin that is maximising the number of seats or
at least maximising revenue from the seats, bearing in mind that
sleeper seats command a substantial premium with respect to economy
seats.
SUMMARY OF THE INVENTION
[0007] The object of the present invention is to provide an
improved array of aircraft seats
[0008] According to the invention there is provided an array of
aircraft seats comprising: [0009] two columns of seats arranged for
array along an aircraft cabin on respective sides of a longitudinal
axis of the array; [0010] the seats having respective central axes,
[0011] the seats in each column having their central axes angled
with respect to the longitudinal axis, [0012] the seats in one
column being offset along the longitudinal axis with respect to the
corresponding seats in the other column, whereby the intersections
with the longitudinal axis of the central axes of the seats of one
column are interdigitated with the intersections with the
longitudinal axis of the central axes of the seats of the other
column and [0013] minor, overlapping, inner-end portions of any two
seats arranged for-and-aft of each other in one column extending
across the longitudinal axis from their major portions at their
intersections and an intervening seat in the other column having a
minor, overlapping, inner-end portion extending oppositely across
the longitudinal axis from its major portion at its intersection;
and [0014] a serpentine divider extending generally along the
longitudinal axis between the seats of the two columns, following
the extent of the minor overlapping portions across the
longitudinal axis.
[0015] Preferably, the seats are sleeper seats.
[0016] Whilst non-symmetrical arrangements can be envisaged, in the
preferred embodiments, the minor, overlapping, inner-end portions
of the two columns overlap the longitudinal axis by equal
extents.
[0017] Preferably, the extent of the overlap of the minor,
overlapping, inner-end portions is between 3% and 6% of the overall
width of the array.
[0018] Again in the preferred embodiments, all the seats are
arranged with their central axes at substantially the same angle
with respect to the longitudinal axis.
[0019] In one preferred embodiment, the seats are arranged in a
staggered chevron array, that is with the seats in one column
angled with respect to the seats in the other column, and with the
central axes of all the seats in one column making with the
longitudinal axis substantially the same angle measured in the
clockwise (or anti-clockwise) direction as the central axes of all
the seats in the other column make with the longitudinal axis
measured in the anti-clockwise (or clockwise) direction.
[0020] In a staggered chevron array, the seats all face in the same
direction with respect to the column axis, and preferably outwards
of the array, that is with their portions extending across the axis
being at the head ends of the seats. Preferably, the array is
arranged so that the seats are forwards and outwards facing in the
aircraft cabin.
[0021] In another embodiment, known as the "parallel array", the
seats in one column face in one direction and the seats in the
other column face in the other direction and again all preferably
outwards. Whilst each seat in one column could be aligned with an
oppositely facing seat in the other column, they are preferably
offset from each other.
[0022] Preferably, the array includes on opposite sides of aisles
outboard of the two columns of seats, two side columns of angled
seats are set against cabin side walls, one side column on one side
of the two column array along the longitudinal axis and the other
on the other side. Normally these seats will be both outwards and
forwards facing.
BRIEF DESCRIPTION OF THE DRAWINGS
[0023] To help understanding of the invention, a specific
embodiment thereof will now be described by way of example and with
reference to the accompanying drawings, in which:
[0024] FIG. 1 is a plan view of a short array of four sleepers
seats arrayed in first embodiment in accordance with the
invention;
[0025] FIG. 2 is a LOPA view of the seats of FIG. 1 in an aircraft
cabin;
[0026] FIG. 3 is an equivalent LOPA to that of FIG. 2 showing a
cabin equipped with conventional seats;
[0027] FIG. 4 is a plan view of a short array of four sleepers
seats arrayed in second embodiment in accordance with the
invention; and
[0028] FIG. 5 is a LOPA view of the seats of FIG. 1 in another
aircraft cabin; and
[0029] FIG. 6 is an equivalent LOPA to that of FIG. 5 showing a
cabin equipped with conventional seats.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT
[0030] Referring to FIGS. 1 & 2, the sleeper seats 1 are shown
there in sleeping mode. Each comprises a head rest 2, a back rest
3, a seat pan or seat cushion 4 and a leg rest 5, all of which move
in a conventional manner when the seat is moved from sleeping mode
to sitting mode. The seats also include ottomans 6 and dividers 7
between the individual seats with the their column. The four seats
shown in FIG. 1 are arranged in a staggered chevron formation and
two columns 8, 9. All the seats in each column are parallel with
each other and set at a "herringbone" angle .alpha. to the column
direction, in other words their central axes A make the angle
.alpha. with a longitudinal axis 10 of the array. The seats being
arranged in the staggered chevron array, the seats in one column
are angled with respect to the seats in the other column, and the
central axes of all the seats in one column make with the
longitudinal axis substantially the same angle measured in the
clockwise (or anti-clockwise) direction as the central axes of all
the seats in the other column make with the longitudinal axis
measured in the anti-clockwise (or clockwise) direction.
[0031] Each seat extends from its column side of the longitudinal
axis across the axis to a small extent 11. Along the axis, first a
seat from one column crosses the axis and then a seat from the
other column crosses the axis and so on. The seats on opposite
sides of the axis are screened from each other by a serpentine
divider 12, which passes from one side of the axis 10 to the other
side along the longitudinal axis. At joints 15, just on an
individual seat's side of the longitudinal axis, the serpentine
divider forks from the seat's own divider 7 from the next seat in
the respective column. In effect the serpentine divider is
comprised of successive longitudinal axis portions 15 of the
dividers 7, which are made as a continuous piece from their inboard
ends 16 to their outboard ends 17.
[0032] In addition to the seats extending to the small extent 11
across the longitudinal axis, bed side areas 18 at end 19 also
extend across the axis.
[0033] Typically for a herringbone angle .alpha. of 34.degree. and
an array width 20 of 93.5 inches (2375 mm), the extent of the
overlap is 3.3 inches (84 mm) in the widthwise direction, i.e. 3.5%
of the array width. In another example (not illustrated) for an
array of 85.4 inches (2169 mm) and a herringbone angle of
30.degree. the overlap is also 3.9 inches (99 mm), i.e. 4.6% of the
array width.
[0034] As shown in FIG. 2, which is a three class/fare LOPA, the
seats 1 arrayed in accordance with the invention are installed in a
business class section 21 of the cabin. Similar, single column,
herringbone arrayed seats 51 are provided along the side wall 52 of
the cabin.
[0035] It can be noted that array of FIG. 1 has advantages, which
can be appreciated from FIG. 2 by comparison with FIG. 3, which
shows an equivalent business class passenger count LOPA, it is
necessary to utilise conventional business class seats 22 arrayed
three abreast along the centre of the cabin. This requires central
passengers to step over their neighbours for aisle access, as is
required window seat passengers seated against the side wall of the
cabin. By contrast, the seats 1 arrayed in accordance with the
invention all have direct aisle access. Further, it will be noted
that the array in accordance with the invention allows an increase
by sixteen in the number of economy class seats 23.
[0036] Turning now to FIGS. 4 & 5, again the sleeper seats 101
are shown there in sleeping mode. Each comprises a head rest 102, a
back rest 103, a seat pan or seat cushion 104, an ottoman 105, a
foot rest 106 and a divider 107 analogous to those of the first
embodiment. Again the seats are arranged on both sides of the
longitudinal axis 110 in two columns 108,109. However, they are all
parallel to each other as opposed to being arranged in chevron
formation. The central axes A of all the seats in both columns make
with the longitudinal axis substantially the same angle .alpha.
measured in the clockwise (or anti-clockwise) direction.
[0037] Again, each seat extends from its column side of the
longitudinal axis across the axis to a small extent 111. Along the
axis, first a seat from one column crosses the axis and then a seat
from the other column crosses the axis and so on. The seats on
opposite sides of the axis are screened from each other by a
serpentine divider 112, again integrated with the inter-seat
dividers.
[0038] The seats on opposite sides of the serpentine dividers are
arranged head to head, but with a slight offset 131 in their own
longitudinal axes 132.
[0039] In addition to the seats extending to the small extent 111
across the longitudinal axis, so do bed side areas 118 at end
119.
[0040] Typically for an array angle .alpha. of 29.degree. and an
array width 120 of 83.5 inches (2121 mm), the extent of the overlap
is 4.6 inches (117 mm) in the widthwise direction, i.e. 5.5% of the
array width.
[0041] Turning now to FIG. 5, which is a two passenger class LOPA,
by comparison with FIG. 6 with an equivalent conventional in line
business class cabin, the array in accordance with this embodiment
of the invention, again allows an increase in the total number of
passengers accommodated.
* * * * *